摘要
建立了火箭弹／火箭炮系统的相互作用动力学模型，并通过计算机模拟，得到了某火箭武器系统的发射架运动与火箭弹弹道偏差的函数关系，为优选火箭点火时间以提高无控火箭射击密集度提供了基础。
A interaction dynamical model of rocket/launcher systim are reported in this paper.By computer simuiation,the quantitative reiation between launcher motion and rocket trajectory errors is published.And it is the basis of increasing fining concentration of non-controlling rockets by optimizing ignitiontime.
出处
《弹道学报》
CSCD
1994年第3期62-67,共6页
Journal of Ballistics
